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Burst vortex/boundary layer interactionSeveral configurations of delta wing vortex generator and boundary layer test plate were tested, and two final ones selected. Sample measurements and flow visualizations in the candidate configurations, together with more detailed measurements in one of the two final arrangements, which were selected so that a pure vortex bursts repeatably and then interacts, in as simple fashion as possible, with a simple turbulent boundary layer, are included. It is concluded that different intensities of bursting or breakdown, like different strengths of shock wave or hydraulic jump, can be produced by minor changes of configuration. The weaker breakdowns do not produce flow reversal. The initial measurements were done with a fairly weak, but repeatable, breakdown. Basic measurements on the second final arrangement, with a stronger breakdown, are in progress.
Document ID
19880008199
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bradshaw, P.
(Imperial Coll. of Science and Technology London, United Kingdom)
Naaseri, M.
(Imperial Coll. of Science and Technology London, United Kingdom)
Date Acquired
September 5, 2013
Publication Date
March 14, 1988
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:182510
NASA-CR-182510
Report Number: NAS 1.26:182510
Report Number: NASA-CR-182510
Accession Number
88N17583
Funding Number(s)
CONTRACT_GRANT: NAGW-581
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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